titanium & titanium alloys - lawrence berkeley national laboratory

21
Titanium & Titanium Alloys AMS Properties 4900L Sheet, Strip and Plate, C.P., Annealed, 55.0 ksi (379 MPa) Yield Strength 4901M Sheet, Strip, and Plate, C.P. Annealed, 70.0 ksi (485MPa)<=:p> 4902G Sheet, Strip, and Plate, C.P. Annealed, 40.0 ksi (276 MPa) Yield Strength 4905B Damage-Tolerant Grade Plate 6AL – 4V, Beta, Annealed=o:p> 4907F Sheet, Strip, and Plate 6AL-4V, Extra Low Interstitial Annealed 4908F Sheet and Strip, 8Mn, Annealed, 110,000 psi (760 MPa) Yield Strength 4909F Sheet, Strip, and Plate 5AL -2.5Sn, Extra Low Interstitial, Annealed 4910K Sheet, Strip and Plate 5AL – 2.5Sn Annealed 4911H Sheet, Strip, and Plate, 6AL – 4V, Annealed 4914A Cold Rolled Sheet and Strip, 15V - 3AL – 3Cr –=3Sn Solution Heat Treated 4915G Sheet, Strip, and Plate, 8AL – 1V – 1Mo, Single Annealed 4916F Sheet, Strip, and Plate, 8AL – 1Mo – 1V, Duplex Annealed 4917E Sheet, Strip, and Plate, 13.5V – 11Cr – 3.0AL, Solution Heat Treated 4918H Sheet, Strip, and Plate, 6AL – 6V- 2Sn Annealed 4919C Sheet, Strip, and Plate, 6AL– 2Sn – 4Zr – 2M0 – 0.08Si, Duplex Annealed 4920B Forgings, 6AL – 4V, Alpha-Beta or Beta Processed, Annealed 4921G Wire, Forgings, and Rings C.P. 70.0 ksi (438 MPa) Yield Strength 4924D Bars, Forgings, and Rings 5AL – 2.5Sn, Extra Low Interstitial, Annealed 4926J Bars, Wire, and Rings, 5AL – 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength 4928Q Bars, Wire, Forgings, Rings, and Drawn Shapes 6AL – =V Annealed 4930E Bars, Wire, Forgings, and Rings, 6AL – 4V, Extra Low Interstitial Annealed 4931A Bars, Forgings, & Rings 6AL – 4V Extra Low Interstitial (ELI) Duplex

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Page 1: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

Titanium & Titanium AlloysAMS Properties

4900L Sheet, Strip and Plate, C.P., Annealed, 55.0 ksi (379 MPa) Yield Strength

4901M Sheet, Strip, and Plate, C.P. Annealed, 70.0 ksi (485MPa)<=:p>

4902G Sheet, Strip, and Plate, C.P. Annealed, 40.0 ksi (276 MPa) Yield Strength

4905B Damage-Tolerant Grade Plate 6AL – 4V, Beta, Annealed=o:p>

4907F Sheet, Strip, and Plate 6AL-4V, Extra Low Interstitial Annealed

4908F Sheet and Strip, 8Mn, Annealed, 110,000 psi (760 MPa) Yield Strength

4909F Sheet, Strip, and Plate 5AL -2.5Sn, Extra Low Interstitial, Annealed

4910K Sheet, Strip and Plate 5AL – 2.5Sn Annealed

4911H Sheet, Strip, and Plate, 6AL – 4V, Annealed

4914A Cold Rolled Sheet and Strip, 15V - 3AL – 3Cr –=3Sn Solution Heat Treated

4915G Sheet, Strip, and Plate, 8AL – 1V – 1Mo, Single Annealed

4916F Sheet, Strip, and Plate, 8AL – 1Mo – 1V, Duplex Annealed

4917E Sheet, Strip, and Plate, 13.5V – 11Cr – 3.0AL, Solution Heat Treated

4918H Sheet, Strip, and Plate, 6AL – 6V- 2Sn Annealed

4919C Sheet, Strip, and Plate, 6AL– 2Sn – 4Zr – 2M0 – 0.08Si, Duplex Annealed

4920B Forgings, 6AL – 4V, Alpha-Beta or Beta Processed, Annealed

4921G Wire, Forgings, and Rings C.P. 70.0 ksi (438 MPa) Yield Strength

4924D Bars, Forgings, and Rings 5AL – 2.5Sn, Extra Low Interstitial, Annealed

4926JBars, Wire, and Rings, 5AL – 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength

4928Q Bars, Wire, Forgings, Rings, and Drawn Shapes 6AL – =V Annealed

4930E Bars, Wire, Forgings, and Rings, 6AL – 4V, Extra Low Interstitial Annealed

4931A Bars, Forgings, & Rings 6AL – 4V Extra Low Interstitial (ELI) Duplex

Page 2: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

4933BExtrusions and Flash Welded Rings, 8AL – 1Mo –=1V, Solution Heat Treated & Stabilized

4934C Extrusions and Flash Welded Rings 6AL – 4V Solution =eat Treated and Aged

4935F Extrusions and Flash Welded Rings, 6AL – 4V, Anneale=, Beta Processed

4936DExtrusions and Flash Welded Rings, 6AL – 6V – =Sn, Beta Extruded Plus Annealed, Heat Treatable

4937AExtrusions and Flash Welded Rings 6AL –6V – 2Sn Beta Extruded Plus Annealed, Heat Treatable

4941C Tubing, Welded, Annealed, 40,000 psi (275 MPa) Yield Stren=th

4942D Tubing, Seamless, Annealed, 40,000 psi (275 MPa) Yield Strength

4943F Hydraulic, Seamless Tubing 3.0AL – 2.5V Annealed

4944F Seamless, Hydraulic Tubing 3.0AL – 2.5V Cold Worked, Stress Relieved

4945BTubing, Seamless, Hydraulic, 3AL – 2.5V, Texture Controlled, 105 ksi (724 Mpa)Yield Strength Cold Worked, Stress Relieved<=:p>

4950Bars, Wire, Forgings, and Rings 6.0AL – 4.0V Solution Heat Treated & Aged Modified Strength

4951F Welding Wire, C.P. Environment Controlled Packaging

4952A Welding Wire, 6AL – 2Sn – 4Zr – 2Mo

4953C Welding Wire. 5AL – 2.5Sn

4954F Welding Wire, 6AL – 4V

4955D Welding Wire, 8AL – 1Mo – 1V=/p>

4956CWelding Wire, 6AL – 4V, Extra Low Interstitial, Environment Controlled Packaging

4957BRound Bar and Wire, 3AL – 8V – 6Cr – 4Mo – 4Zr, Consumable Electrode Melted, Solution Heat Treated & Cold Drawn

4958ABars and Rods, 3AL – 8V – 6Cr – 4Mo R=1; 4Zr, Consumable Electrode Melted, Solution Heat Treated & Centerless Ground

4959C Wire, 13.5V – 11Cr – 3AL, Spring Temper

4963Bars, Wire, Forgings, and Rings 6AL – 4V Annea=ed, Heat Treatable, Modified Strength

4965G Bars, Wire, Forgings, and Rings 6AL – 4V Solution He=t Treated & Aged

Page 3: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

4966L Forgings 5AL – 2.5Sn Annealed, 110 ksi (758 MPa) Yie=d Strength

4967H Bars, Wire, Forgings, and Rings 6AL – 4V, Annealed, =eat Treatable

4970F Bars, Wire, and Forgings 7AL – 4Mo, Solution & Precipitation Heat Treated

4971E Bars, Wire, Forgings, and Rings 6AL – 6V – 2Sn Annealed, Heat Treatable

4972D Bars, Wire, and Rings, 8AL – 1Mo – 1V, Solution Heat Treated & Stabilized

4973D Forgings, 8AL – 1Mo – 1V, Solution Heat Treated & Stabilized

4974CBars, and Forgings, 11Sn – 5.0Zr – 2.3AL =; 1.0Mo – 0.21Si, Solution &̵ Precipitation Heat Treated

4975GBars, Wire, & Rings, 6.0AL – 2.0Sn – 4.0Zr – 2.oMo – 0.08Si, Solution & Precipitation Heat Treated

4976E Forgings, 6AL – 2Sn – 4Zr – 2Mo, Solution & Precipitation Heat Treated

4978C Bars, Wire, Forgings, and Rings, 6AL – 6V – 2S=, Annealed

4979DBars, Wire, Forgings, and Rings 6AL - 6V – 2Sn Solut=on & Precipitation Heat Treated

4981CBars, Wire, and Forgings, 6AL– 2Sn – 4Zr =; 6Mo, Solution & Precipitation̵ Heat Treated

Titanium ASTM Specifications

ASTM-F136-98e1Wrought Titanium-6 Aluminum-4 Vanadium ELI (Extra Low Interstitial) Alloy (UNSR56401) for Surgical Implant Applications

ASTM-F67-00Unalloyed Titanium for Surgical Implant Applications (UNS R50250, UNS R50400, UNS R50550, UNS R50700)

ASTM-F1108-97aTi6AL4V Alloy Castings for Surgical Implants (UNS R56406)<=:p>

ASTM-F-620-00Alpha Plus Beta Titanium Alloy Forgings for Surgical Impla=ts

ASTM-F1472-99Wrought Titanium-6 Aluminum-4 Alloy for Surgical Implant Applications (UNS R56400)

ASTM-F1341-99Unalloyed Titanium Wire UNS R50250, UNS R50400, UNS R50550, UNS R50700, for Surgical Implant Applications

Page 4: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

ASTM-F1295-97a Wrought Titanium-6 Aluminum-7 Niobium Alloy for Surgical Implant Applications (UNS R56700)

ASTM B265-99 Titanium and Titanium Alloy Strip, Sheet, and Plate

ASTM-B299-99 Titanium Sponge

ASTM-B338-99Seamless and Welded Titanium &Titanium Alloy Tubes for Condensers & Heat Exchangers

ASTM-B348-00 Titanium and Titanium Alloy Bars and Billets

ASTM-B363-00Seamless and Welded Unalloyed Titanium & Titanium Alloy Welding Fittings

ASTM-B367-93 (1998) Titanium and Titanium Alloy Castings

ASTM-B381-00 Titanium and Titanium Alloy Forgings

ASTM-B600-91 (1997)e1Standard Guide for Descaling and Cleaning Titanium & Titanium Alloy Surfaces

ASTM-B861-00 Titanium and Titanium Alloy Seamless Pipe

ASTM-B862-99 Titanium and Titanium Alloy Welded Pipe

ASTM-B863-99a Titanium and Titanium Alloy Wire

Page 5: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

ASTM Tensile Requirements (Bar, billet)

1 35 240 25 170 24 30

2 50 345 40 275 20 30

3 65 450 55 380 18 30

4 80 550 70 483 15 25

5 130 895 120 828 10 25

6 120 828 115 795 10 25

7 50 345 40 275 20 30

9 90 620 70 483 15 25

9B 90 620 70 483 12 25

11 35 240 25 170 24 30

12 70 483 50 345 18 25

13 40 275 25 170 24 30

14 60 410 40 275 20 30

15 70 483 55 380 18 25

16 50 345 40 275 20 30

17 35 240 25 170 24 30

18 90 620 70 483 15 25

18B 90 620 70 483 12 20

19C 115 793 110 759 15 25

19D 135 930 130 to 159897 to 1096

10 20

19E 165 1138 160 to 1851104 to 1276

5 20

20C 115 793 110 759 15 25

Page 6: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

21C 115 793 110 759 15

21D 140 966 130 to 159 897 to 1096 10

21E 170 1172 160 to 1851104 to 1276

8

23 120 828 110 759 10

23B 120 828 110 759 7.5F,6.0G

24 130 895 120 828 10

25 130 895 120 828 10

26 50 345 40 275 20

27 35 240 25 170 24

28 90 620 70 483 15

28B 90 620 70 483 12

29 120 828 110 759 10

29B 120 828 110 759 7.5F,6.0G

30 50 345 40 275 20

31 65 450 55 380 18

32 100 689 85 586 10

33 50 345 40 275 20

34 65 450 55 380 18

These properties =pply to longitudinal sections up to 3 in (76mm) in thickness with maximum o= 10 in. 2(64.5cm2). Mechanical properties of larger sections shall be negotiated between the manufacturer and purchaser.

B- Properties for material in transformed-b=ta condition.

C- Properties for solution treated condition

Page 7: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

D- Properties for solution treated and aged condition-Moderate strength (determined by aging temperature).

E- Properties for solution treated and aged condition-High strength (determined by aging temperature).

F- For product section or wall thickness va=ues < 1.0 in.

G- For product section or wall thickness values_> 1.0 in.

Page 8: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

ASTM Tensile Strength Requirements(Sheet & Plate)

Minimum and maxim=m limits apply to tests taken both longitudinal and transverse to the direction of rolling. Mechanical properties for conditions other than annealed or plate thickness over 1 in. (25 mm) may be established=by agreement between the manufacturer and the purchaser.

B- T equals the thickness of the bend test specimen. Bend tests are not applicable to material over 0.187 in (4.75 min) in thickness.

C- For Grades 5, 6 and 32 the elongation on materials under 0.025 in. (0.635 mm) in thickness may be obtained only=by negotiation.D- Elongation for continuous rolled and ann=aled (strip product from coil) for Grade 9 and Grade 18 shall be 12% minimu= in the longitudinal direction and 8% minimum in the transverse direction.=br>

E- Properties for material in the solution treated condition.F- Material is normally purchased in the so=ution treated condition.Therefore, properties for aged material shall=be negotiated between manufacturer and purchaser.

AMS

Properties

1 35 240 25 170 45 310 24 3T 4T2 50 345 40 275 65 450 20 4T 5T3 65 450 55 380 80 550 18 4T 5T4 80 550 70 483 95 655 15 5T 6T5 130 895 120 828 ... ... 10C 9T 10T6 120 828 115 793 ... ... 10C 8T 9T7 50 345 40 275 65 450 20 4T 5T9 90 620 70 483 ... ... 15D 5T 6T11 35 240 25 170 45 310 24 3T 4T12 70 483 50 345 ... ... 18 4T 5T13 40 275 25 170 ... ... 24 3T 4T14 60 410 40 275 ... ... 20 4T 5T15 70 483 55 380 ... ... 18 4T 5T16 50 345 40 275 65 450 20 4T 5T17 35 240 25 170 45 310 24 3T 4T18 90 620 70 483 ... ... 15D 5T 6T19E,F 115 793 110 759 ... ... 15 6T 6T20E,F 115 793 110 759 ... ... 15 6T 6T21E,F 115 793 110 759 ... ... 15 6T 6T23E,F 120 828 110 759 ... ... 10 9T 10T24 130 895 120 828 ... ... 1025 130 895 120 828 ... ... 1026 50 345 40 275 65 450 20 4T 5T27 35 240 25 170 45 310 24 3T 4T28 90 620 70 483 ... ... 15 5T 6T29 120 828 110 759 ... ... 10 9T 10T30 50 345 40 275 65 450 20 4T 5T31 65 450 55 380 80 550 18 4T 5T32 100 689 85 586 ... ... 10C 7T 9T33 50 345 40 275 65 450 20 4T 5T34 65 450 55 380 80 550 18 4T 5T

Page 9: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

4900L Sheet, Strip and Plate, C.P., Annealed, 55.0 ksi (379 MPa) Yield Strength

4901M Sheet, Strip, and Plate, C.P. Annealed, 70.0 ksi (485MPa)<=:p>

4902G Sheet, Strip, and Plate, C.P. Annealed, 40.0 ksi (276 MPa) Yield Strength

4905B Damage-Tolerant Grade Plate 6AL – 4V, Beta, Annealed=o:p>

4907F Sheet, Strip, and Plate 6AL-4V, Extra Low Interstitial Annealed

4908F Sheet and Strip, 8Mn, Annealed, 110,000 psi (760 MPa) Yield Strength

4909F Sheet, Strip, and Plate 5AL -2.5Sn, Extra Low Interstitial, Annealed

4910K Sheet, Strip and Plate 5AL – 2.5Sn Annealed

4911H Sheet, Strip, and Plate, 6AL – 4V, Annealed

4914A Cold Rolled Sheet and Strip, 15V - 3AL – 3Cr –=3Sn Solution Heat Treated

4915G Sheet, Strip, and Plate, 8AL – 1V – 1Mo, Single Annealed

4916F Sheet, Strip, and Plate, 8AL – 1Mo – 1V, Duplex Annealed

4917E Sheet, Strip, and Plate, 13.5V – 11Cr – 3.0AL, Solution Heat Treated

4918H Sheet, Strip, and Plate, 6AL – 6V- 2Sn Annealed

4919C Sheet, Strip, and Plate, 6AL– 2Sn – 4Zr – 2M0 – 0.08Si, Duplex Annealed

4920B Forgings, 6AL – 4V, Alpha-Beta or Beta Processed, Annealed

4921G Wire, Forgings, and Rings C.P. 70.0 ksi (438 MPa) Yield Strength

4924D Bars, Forgings, and Rings 5AL – 2.5Sn, Extra Low Interstitial, Annealed

4926J Bars, Wire, and Rings, 5AL – 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength

4928Q Bars, Wire, Forgings, Rings, and Drawn Shapes 6AL – =V Annealed

4930E Bars, Wire, Forgings, and Rings, 6AL – 4V, Extra Low Interstitial Annealed

4931A Bars, Forgings, & Rings 6AL – 4V Extra Low Interstitial (ELI) Duplex Annealed, Fracture Toughness<=p>

4933B Extrusions and Flash Welded Rings, 8AL – 1Mo –=1V, Solution Heat

4934C Extrusions and Flash Welded Rings 6AL – 4V Solution =eat Treated and Aged

4935F Extrusions and Flash Welded Rings, 6AL – 4V, Anneale=, Beta Processed Treated & Stabilized

Page 10: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

4936D Extrusions and Flash Welded Rings, 6 H

4937A Extrusions and Flash Welded Rings 6AL –6V – 2Sn Beta Extruded Plus Annealed, Heat Treatable

4941C Tubing, Welded, Annealed, 40,000 psi (275 MPa) Yield Stren=th

4942D Tubing, Seamless, Annealed, 40,000 psi (275 MPa) Yield Strength

4943F Hydraulic, Seamless Tubing 3.0AL – 2.5V Annealed

4944F Seamless, Hydraulic Tubing 3.0AL – 2.5V Cold Worked, Stress Relieved

4945BTubing, Seamless, Hydraulic, 3AL – 2.5V, Texture Controlled, 105 ksi (724 Mpa)Yield Strength Cold Worked, Stress Relieved<=:p>

4950 Bars, Wire, Forgings, and Rings 6.0AL – 4.0V Solution Heat Treated & Aged Modified Strength

4951F Welding Wire, C.P. Environment Controlled Packaging

4952A Welding Wire, 6AL – 2Sn – 4Zr – 2Mo

4953C Welding Wire. 5AL – 2.5Sn

4954F Welding Wire, 6AL – 4V

4955D Welding Wire, 8AL – 1Mo – 1V=/p>

4956C Welding Wire, 6AL – 4V, Extra Low Interstitial, Environment Controlled Packaging

4957B Round Bar and Wire, 3AL – 8V – 6Cr – 4Mo – 4Zr, Consumable Electrode Melted, Solution Heat Treated & Cold Drawn

4958ABars and Rods, 3AL – 8V – 6Cr – 4Mo R=1; 4Zr, Consumable Electrode Melted, Solution Heat Treated & Centerless Ground

4959C Wire, 13.5V – 11Cr – 3AL, Spring Temper

4963 Bars, Wire, Forgings, and Rings 6AL – 4V Annea=ed, Heat Treatable, Modified Strength

4965G Bars, Wire, Forgings, and Rings 6AL – 4V Solution He=t Treated & Aged

4966L Forgings 5AL – 2.5Sn Annealed, 110 ksi (758 MPa) Yie=d Strength

4967H Bars, Wire, Forgings, and Rings 6AL – 4V, Annealed, =eat Treatable

4970F Bars, Wire, and Forgings 7AL – 4Mo, Solution & Precipitation Heat Treated

4971E Bars, Wire, Forgings, and Rings 6AL – 6V – 2Sn Annealed, Heat Treatable

4972D Bars, Wire, and Rings, 8AL – 1Mo – 1V, Solution Heat Treated & Stabilized

Page 11: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

4973D Forgings, 8AL – 1Mo – 1V, Solution Heat Treated & Stabilized

4974C Bars, and Forgings, 11Sn – 5.0Zr – 2.3AL =; 1.0Mo – 0.21Si, Solution & Precipitation Heat Treated̵

4975G Bars, Wire, & Rings, 6.0AL – 2.0Sn – 4.0Zr – 2.oMo – 0.08Si, Solution & Precipitation Heat Treated

4976E Forgings, 6AL – 2Sn – 4Zr – 2Mo, Solution & Precipitation Heat Treated

4978C Bars, Wire, Forgings, and Rings, 6AL – 6V – 2S=, Annealed

4979D Bars, Wire, Forgings, and Rings 6AL - 6V – 2Sn Solut=on & Precipitation Heat Treated

4981C Bars, Wire, and Forgings, 6AL– 2Sn – 4Zr =; 6Mo, Solution & Precipitation Heat Treated̵

Page 12: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

Titanium MIL-T SpecificationsAMS-T-9046(Issued 1999

APPLICABLE DOCUMENTS

Commercially Pure Titanium

(CP) CODE Yield Strength (min. ksi) MIL-H-81200Heat Treatment of Titanium and Titanium Alloys<=span>

CP-1 (70 KSI-YS) FED-STD-151 Metals, Test Methods

CP-2 (55 KSI-YS) MIL-STD-105Sampling Procedures and Tables for Inspection by Attribute=.

CP-3 (40 KSI-YS)

CP-4 (30 KSI-YS) MIL-STD-129Marking for Shipment and Storage

MIL-STD-163Steel Mill Products Preparation for Shipment and Storage

MIL-STD-410

Nondestructive Testing Personnel Qualification and Certification (Eddy Current, Liquid Penetrant, Magnetic Particle, Radiographic and Ultrasonic)

Alphaium Alloys (A)< b>

CODE Composition SAE Publications

A-1 5AL-2.5Sn AMS - 2242

Tolerances-Corrosion and Heat Resistant Steel and Iron Base Alloy Sheet, Strip and Plate and Titanium and Titanium Alloy Sheet, Strip=and Plate

A-2 5AL-2.5Sn (ELI) AMS 2249Chemical Check Analysis Limits- Titanium and Titanium Allo=s

A-3 6AL-2Cb-1Ta-0.8Mo AMS 2631Ultrasonic Inspection of Titanium and Titanium Alloys

A-4 8AL-1Mo-1V ARP 982AMinimizing Stree Corrosion in Wrought Heat Treatable Titan=um Alloys

Alpha-Beta Titanium Alloy< b> ASTM Publications

Page 13: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

(AB) CODE Composition ASTM A 480 General Requirements for Flat Rolled Stainless and Heat Resisting Steels in Form of Plate, Sheet and Strip

AB-1 6AL-4V ASTM E 8Tension Testing of Metallic Materials

AB-2 6AL-4V (ELI) ASTM E 120Titanium and Titanium-Base Alloys, Chemical Analysis of Semi-Guided

AB-3 6AL-6V-2Sn ASTM E 290Bend Test for Ductility of Metallic Materials

AB-4 6AL-2Sn-4Zr-2Mo

AB-5 3.AL-2.5V

AB-6 8Mn

Beta Titanium Alloys (B

CODE Composition

B-1 13V-11Cr-3AL

B-2 11.5Mo-6Zr-4.5Sn

B-3 3AL-8V-6Cr-4Mo-4Zr

B-4 8Mo-8V-2Fe-3AL

NDITION CODE: DESCRIPTION:

A ANNEALED

DA DUPLEX ANNEALED

TA TRIPLEX ANNEALED

ST SOLUTION TREATED

Page 14: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

Military Specifications

Titanium and Titanium Alloy(Sheet-Strip-Plate)

MIL-T-9046H MIL-T-9046J AMENDMENT-2 (1991)<=span>

Type I

Commercially Pure Titanium (CP)=/span>

Code Designation Code Designation

Comp A - Unalloyed

(40 KSI-YS)

CP-3 (40 KSI-YS)

Comp B - Unalloyed

(70 KSI-YS)

CP-1 (70 KSI-YS)

Comp C - Unalloyed

(55 KSI-YS)

CP-2 (55 KSI-YS)

CP-4 (30 KSI-YS)

Type II Alpha Titanium A

Alpha Titanium Alloys (A)<

b>

CodeComposition

Code Composition

Comp A 5AL-2.5Sn A-1 5AL-2.5Sn

Comp B5AL-2.5Sn ELI

A-25AL-2.5Sn (ELI)

Comp F8AL-1Mo-1V

A-36AL-2Cb-1Ta-0.8Mo

Comp G6AL-2CG-1Ta-0.8Mo

A-4 8AL-1Mo-1V

Type IIIAlpha-Beta Titanium

Alloy< b>

Alpha-Beta Titanium Alloy

(AB)<=span>

CodeComposition

Code Composition

Comp C 6AL-4V AB-1 6AL-4V

Comp D6AL-4V ELI

AB-2 6AL-4V (ELI)

Page 15: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

Beta Titanium

Alloys=/p>

Beta Titanium Alloys

(B)=/b>

CodeComposition

Code Composition

Comp A13V-11Cr-3AL

B-1 13V-11Cr-3AL

Comp B11.5Mo-6Zr-4.5Sn

B-211.5Mo-6Zr-4.5Sn

Comp C3AL-8V-6Cr-4Mp 4Zr

B-33AL-8V-6Cr-4Mo-4Zr

Comp D8Mo-8V-2Fe-3AL

B-48Mo-8V-2Fe-3AL

Titanium MIL-T Specifications:Bar & Reforge StockOther Specification:

MIL-H-81200 Rev. B(1991) Heat Treatment of Titanium & Titanium alloys

MIL-T-81556AExtruded Bars & Shapes, Titanium & Titanium alloys=o:p>

MIL-I-8950 Ultrasonic Inspections

AMS-STD 2154(1982) Ultrasonic Inspections

AMS 2241 Rev. L(1996)Tolerances, Titanium & Titanium alloy bars & wire<=:p>

AMS 2242 Rev. E(1995) Tolerances, Titanium sheet & plate

AMS 2244 Rev. B(1994) Tolerances, Titanium tubing

AMS 2245 Rev. A(1994) Tolerances, Titanium extruded bar

AMS 2249 Rev. D(1992)Chemical Check Analysis Limits, Titanium & Titanium al=oys

Page 16: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

AMS 2801 Rev. A(1994)Tolerances, Titanium heat treatment specifications

AMS 2809(1994) Identification Requirements

Properties of Titanium

Atomic Number 22

Heat of Vaporization 9.83MJ/kg

Atomic Weight 47.9

Machinability Rating 40

Atomic Volume 10.6W/D

Magnetic Susceptibility 1.25x10-6 / 3.17 emu/g

Boiling Point 3260 °C/5900 °F

Melting Point 1668°C + 10°C (3035°F + 18°F)

Coefficient of friction0.8 at 40 m/min (125 ft/min) / 0.68 at 300 m/min (1000 ft/=in)

Modulus of Elasticity 14.9 x 106psi

Coefficient of thermal expansion 22

Atomic Number 8.64 x 10-6°C

Poisson's Ratio 0.41

Color Dark Grey

Solidus/Liquidus 1725°C/ (3137°F)

Covalent Radius 1.32 A

Specific Gravity 4.5

Density 4.51 gm/cm3 (0.163 lb/in3)

Specific Heat (at 25oC) 0.518 J/kg °K, (0.124 BTU/lb °F)<=span>

Page 17: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

Electrical Conductivity ]3% IACS (copper 100%)

Specific resistance 554 µohm-cm

Electrical Resistivity 47.8 µohm-cm

Tensile Strength 35 ksi min

Electronegativity 1.5 Pauling's

Thermo-Conductivity 9.0 BTU/hr ft2°F

First Ionization Energy 158 k-cal/g-mole

Thermal Neutron Absorption Cross

Section=/p> 5.6 barnes/atom

Hardness HRB 70 to 74

Young's Modulus of Elasticity 116 x 106 lbf/in2, 102.7 GPA

Heat of Fusion 440 kJ/kg (est.)

Tech Properties of Titanium25 170 35 35 240

40 275 50 345 20 %

55 380 65 450 18

70 485 80 550 15

40 275 50 345 20

50 345 70 483 18

120 830 130 895 10

125 850 170 1160 10

160 1100 180 1250 8

160 1100 185 1280 10

Ti-10-2-3

Ti-15-3

Page 18: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

Ti-6-2-4-2

LengthENGLISH TO METRIC (SI)

METRIC (SI) TO ENGLISH

1 inch (in)

25.4 mm

1 Millimeter (mm)

0.03937 in

2.54 cm 0.003281 ft

0.0254 m 0.001094 yd

1 Foot (ft)

304.800 mm

1 Centimeter (cm)

0.3937 in

30.480 cm 0.03281 ft

0.3048 m 0.01094 yd

1 Yard (yd)

91.4402 cm

1 Meter (m)

39.37 in

0.9144 m 3.2808 ft

0.000914 km 1.0936 yd

0.0005214 mi

1 Mile (mi)

1609.344 m

1 Kilometer (km)

3280.833 ft

1.6093 km 1093.611 yd

0.6214 mi

AREAENGLISH TO METRIC (SI)

METRIC (SI) TO ENGLISH

1 Cir Mil

0.0005067 sq mm

1 sq mm

1,973.55 cir mils

0.001550 sq in

0.00010764 sq ft

0.000001196 sq yd

1 sq inch (in)

645.163 sq mm

1 sq cm

0.1550 sq in

6.4516 sq cm 0.001076 sq ft

0.0006452 sq m 0.000,1196 sq yd

Page 19: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

1 sq foot (ft

92,903.41 sq mm

1 sq

1,549.9969 sq in

929.0341 sq.cm 10.7639 sq ft

0.0929 sq m 1.1960 sq yd

0.000929 sq km 0.0003861 sq mi

1 sq Yard (yd)

836,130.74 sq mm

1 sq km

10,763,867.36 sq ft

8,361.307 sq cm 1,195,985.26 sq yd

0.83613 sq m 0.3861 sq mi

0.000836 sq km

Hardness Conversion TableRockwell Rockwel

rdness B Scale C Scale

653 - 62 324,000 217 95 103,000

627 - 60 311,000 212 96 103,000

601 - 68 306,000 207 95 101,000

578 - 57 290,000 202 94 98,000

555 - 56 284,000 197 93 96,000

534 - 54 270,000 192 92 93,000

514 - 53 263,000 187 91 91,000

495 - 51 250,000 183 90 89,000

477 - 50 243,000 179 89 87,000

461 - 49 236,000 174 88 85,000

Page 20: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

429 - 47 217,000 166 86 81,000

415 - 45 211,000 163 85 80,000

401 - 42 194,000 159 84 78,000

388 - 41 188,000 156 83 77,000

375 - 40 182,000 153 82 76,000

363 - 38 171,000 149 81 75,000

352 - 37 166,000 146 80 74,000

331 - 36 162,000 143 79 73,000

321 - 34 153,000 140 78 71,000

311 - 33 148,000 137 77 70,000

302 - 32 144,000 134 76 69,000

293 - 31 140,000 131 74 67,000

285 - 30 136,000 128 73 66,000

277 - 29 132,000 126 72 65,000

269 - 28 129,000 124 71 63,000

262 - 27 126,000 121 70 62,000

255 - 25 120,000 118 69 61,000

248 - 24 117,000 116 68 60,000

241 100 23 115,000 114 67 59,000

235 99 22 112,000 112 66 58,000

229 98 21 110,000 109 65 57,000

223 97 20 108,000 107 64 55,000

Page 21: Titanium & Titanium Alloys - Lawrence Berkeley National Laboratory

Gauge ConversionGauge Numbers US Standards Gauge Numbers US Standards

0 0.312 16 0.0625

1 0.281 17 0.0562

2 0.266 18 0.05

3 0.25 19 0.0438

4 0.234 20 0.0375

5 0.219 21 0.0344

6 0.203 22 0.0312

7 0.188 23 0.0281

8 0.172 24 0.025

9 0.156 25 0.0219

10 0.141 26 0.0188

11 0.125 27 0.0172

12 0.109 28 0.0156

13 0.0938 29 0.0141

14 0.0781 30 0.0125